def aircraft_initialization(aircraft, n_pax_ref, design_range, cruise_mach,
propu_config, n_engine):
aircraft_initialize(aircraft, n_pax_ref, design_range, cruise_mach,
propu_config, n_engine)
from marilib.aircraft_model.airplane import viewer as show
#======================================================================================================
# Initialization
#======================================================================================================
propulsive_architecture = 2 # 1:turbofan, 2:partial turboelectric
number_of_engine = 2
aircraft = Aircraft(propulsive_architecture)
n_pax_ref = 150
design_range = unit.m_NM(3000)
cruise_mach = 0.78
#------------------------------------------------------------------------------------------------------
run.aircraft_initialize(aircraft, n_pax_ref, design_range, cruise_mach,
propulsive_architecture, number_of_engine)
#======================================================================================================
# Modify initial values here
#======================================================================================================
aircraft.turbofan_engine.reference_thrust = 118482.
aircraft.wing.area = 152.9
e_power = 1.0e6 # Watts, electric motor power
aircraft.power_elec_chain.mto = e_power
aircraft.power_elec_chain.mcn = e_power
aircraft.power_elec_chain.mcl = e_power
aircraft.power_elec_chain.mcr = e_power
